14.09.2014 Views

On the Formation of Nitrogen Oxides During the Combustion of ...

On the Formation of Nitrogen Oxides During the Combustion of ...

On the Formation of Nitrogen Oxides During the Combustion of ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

5 Results<br />

In general, an increase <strong>of</strong> <strong>the</strong> preheating temperature <strong>of</strong> <strong>the</strong> gas atmosphere<br />

is followed by an increase <strong>of</strong> <strong>the</strong> nitrogen oxide (NO x ) emissions. This is due<br />

to higher effective flame temperatures. However, in <strong>the</strong> lean burning regime,<br />

an increase <strong>of</strong> droplet pre-vaporization results in a decrease <strong>of</strong> NO x emissions<br />

due to <strong>the</strong> reduction in droplet size and in <strong>the</strong> total number <strong>of</strong> burning<br />

droplets acting as hot spots. For conditions close to stoichiometry, <strong>the</strong> effect<br />

<strong>of</strong> pre-vaporization remains moderate, and <strong>the</strong> NO x emissions are almost<br />

independent <strong>of</strong> <strong>the</strong> pre-vaporization rate Ψ. Previous studies <strong>of</strong> Baessler et<br />

al. [31, 32], for instance, showed that a high degree <strong>of</strong> vaporization is required<br />

to achieve a substantial NO x abatement.<br />

In order to achieve a better understanding <strong>of</strong> <strong>the</strong> processes involved, <strong>the</strong> NO x<br />

emissions <strong>of</strong> n-decane (C 10 H 22 ) droplets are discussed and evaluated in detail<br />

on <strong>the</strong> basis <strong>of</strong> experimental and numerical results. The impact <strong>of</strong> <strong>the</strong> ambient<br />

atmosphere, droplet pre-vaporization, preheating, initial droplet size, and<br />

reaction kinetics is investigated. The respective droplet setups and <strong>the</strong> general<br />

conditions were introduced in <strong>the</strong> above Chapters 3 and 4.<br />

For <strong>the</strong> numerical studies presented in <strong>the</strong> following sections, <strong>the</strong> <strong>the</strong>rmophysical<br />

properties <strong>of</strong> <strong>the</strong> liquid fuel are taken from <strong>the</strong> NIST database [311]<br />

and verified with Abramzon and Sazhin [3] and Cuoci et al. [92]. The single<br />

droplet model, as described in Chapters 4.2 and 4.5, is employed with<br />

<strong>the</strong> conduction limit model being used for <strong>the</strong> liquid phase [9, 236, 381–<br />

383, 402, 403, 405]. The initial temperature <strong>of</strong> <strong>the</strong> droplet is set to T 0 = 440 K for<br />

all simulation runs to avoid large heat losses due to heating <strong>of</strong> <strong>the</strong> liquid fuel<br />

and, thus, <strong>the</strong> need to cope with secondary effects. This temperature is 7K<br />

below <strong>the</strong> boiling temperature <strong>of</strong> C 10 H 22 . Moreover, <strong>the</strong> properties <strong>of</strong> <strong>the</strong> gas<br />

phase are calculated from <strong>the</strong> input data <strong>of</strong> <strong>the</strong> chemical reaction mechanism.<br />

The mechanism itself is a combination <strong>of</strong> <strong>the</strong> n-decane kinetics <strong>of</strong> Zhao et al.<br />

[474] and <strong>the</strong> nitrogen oxides chemistry <strong>of</strong> Li and Williams [250]. It was tested<br />

for different flame types in a wide range <strong>of</strong> equivalence ratios (see Chap. 2.3).<br />

155

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!